TY - GEN
T1 - Experimental study on the wing-wake interaction of a flapping wing Micro Aerial Vehicle
AU - Lua, Kim Boon
AU - Jadhav, Siddharth
PY - 2017/6/13
Y1 - 2017/6/13
N2 - This work presents an experimental study of the aerodynamics of different types of wings during the clap-and- peel mechanism on a hovering flapping wing Micro Aerial Vehicle (MAV) platform. A comprehensive analysis of the phenomenon through force measurement, motion capture and flow measurement using Particle Image Velocimetry in a fixed position was performed. The flow field around the two types of wings with identical dimensions but different deformation characteristics is compared to understand the role of their flexibility in enhancing the benefits of clap-and-peel effect. The two wings have different configurations of carbon fiber rod stiffeners. Varying degrees of flexibility along the camber were observed in the two wings. Insights were obtained on the correlation between the chordwise camber of wings and their influence on force generation and energy efficiency of the flapping wing MAV. The relative strength and location of the leading edge vortices were compared. One of the wings exhibited higher average lift force by 32% and higher average power efficiency by 18% than the other. For Particle Image Velocimetry, Rhodamine-B fluorescent particles were used to seed the flow, over the conventional fog and oil droplets. This mitigated the optical obstruction due to reflection of the wing through the use of optical filters on camera lens.
AB - This work presents an experimental study of the aerodynamics of different types of wings during the clap-and- peel mechanism on a hovering flapping wing Micro Aerial Vehicle (MAV) platform. A comprehensive analysis of the phenomenon through force measurement, motion capture and flow measurement using Particle Image Velocimetry in a fixed position was performed. The flow field around the two types of wings with identical dimensions but different deformation characteristics is compared to understand the role of their flexibility in enhancing the benefits of clap-and-peel effect. The two wings have different configurations of carbon fiber rod stiffeners. Varying degrees of flexibility along the camber were observed in the two wings. Insights were obtained on the correlation between the chordwise camber of wings and their influence on force generation and energy efficiency of the flapping wing MAV. The relative strength and location of the leading edge vortices were compared. One of the wings exhibited higher average lift force by 32% and higher average power efficiency by 18% than the other. For Particle Image Velocimetry, Rhodamine-B fluorescent particles were used to seed the flow, over the conventional fog and oil droplets. This mitigated the optical obstruction due to reflection of the wing through the use of optical filters on camera lens.
KW - Biologically Inspired UAS
KW - Energy Efficient UAS
KW - Fluid Structure Interaction
KW - Micro- and Mini- UAS
KW - Particle Image Velocimetry
UR - http://www.scopus.com/inward/record.url?scp=85034039036&partnerID=8YFLogxK
U2 - 10.1109/ICUAS.2017.7991493
DO - 10.1109/ICUAS.2017.7991493
M3 - Conference contribution
AN - SCOPUS:85034039036
T3 - 2017 International Conference on Unmanned Aircraft Systems, ICUAS 2017
SP - 1292
EP - 1301
BT - 2017 International Conference on Unmanned Aircraft Systems, ICUAS 2017
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 2017 International Conference on Unmanned Aircraft Systems, ICUAS 2017
Y2 - 13 June 2017 through 16 June 2017
ER -
